As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BLEED 1 LEAK CLIMBING OUT OF 6,000 AND CABIN ALT CONTINUED TO CLIMB. REMOVED PACK 1 PANEL IAW 06-41-01 OF AMM. PERFORMED GVI OF PACK 1 FOUND COUPLER ABOVE ACM LEAKING ISOLATED PACK 1 AND RAN ENGINE FOR 5 MIN IAW GHC WITH BLEED 1 SELECTED NO MESSAGES NOTED. REMOVED AND REPLACED UPPER AND LOWER DUCT COUPLER SLEEVES IAW AMM 21-51-02-420-002-A. OPS CHECK GOOD IAW MM CH 49-10-00.